Numerical Determination of the Gas-Dynamic Behavior of Vane Cascades with Various Deflection Angles of the Trailing Edges of Longitudinal Ribs of an Advanced Gas-Turbine Engine Thrust Reverser

摘要

The work comprises numerical investigation of the influence of the deflection angles of the trailing edges of longitudinal ribs on the gas-dynamic behavior of vane cascades of a thrust reverser located in the secondary flow of a bypass turbofan engine (BTFE). Verification of the numerical model was performed on the basis of experimental research.